Abstract
In this chapter, geometrically nonlinear FE models, including RVK5, MRT5, LRT5 and LRT56, are validated by static analysis of composite laminated thin-walled structures. Later, the geometrically nonlinear FE models are test by buckling and post-buckling analysis of cylindrical composite panels. Afterwards, the geometrically nonlinear FE models are implemented into static and dynamic analysis of piezolaminated beam, plate and shell structures. In the last part, the simulations of nonlinear phenomena including both geometrically and electroelastic materially nonlinear effects are performed through piezo structures undergoing large displacement and under strong electric field.
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Zhang, SQ. (2021). Nonlinear Analysis of Piezoceramic Laminated Structures. In: Nonlinear Analysis of Thin-Walled Smart Structures. Springer Tracts in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-9857-9_6
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DOI: https://doi.org/10.1007/978-981-15-9857-9_6
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